Fuselage sections (300) having tapered wing rib interfaces (306) are disclosed. A disclosed example apparatus includes a rib (306) associated with a fuselage section (300), and a wing interface surface defined by the rib (306), where the wing interface surface is tapered relative to a longitudinal axis (330) of the fuselage section from an aft end of the fuselage section (300) to a fore end of the fuselage section (300).
FUSELAGE SECTIONS HAVING TAPERED WING RIB INTERFACES
RUMPFSEKTIONEN MIT KONISCHEN FLÜGELRIPPENSCHNITTSTELLEN
SECTIONS DE FUSELAGE AYANT DES INTERFACES DE NERVURE D'AILE CONIQUES
2021-04-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Wing-fuselage interference and tapered wing roots for low-wing monoplanes
Engineering Index Backfile | 1936
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